HP d212 Manual do Utilizador descarregar pdf (Página 21)

FMS-D212-725-1

Page 1-12

This document is private and confidential and is supplied on the express condition that it is not to be used for any

purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.

Revision:

TC Approved Date: 10.05.12

1.6.2.2 Lateral Center of Gravity

Lateral CG limits are 4.7 inches (119.4 millimeters) left and 6.5 inches (165.1

millimeters) right of fuselage centerline.

1.7 Airspeed

7500 pounds (3402 kilograms) GW – V

125 KIAS.

10,500 pounds (4763 kilograms) GW – V

105 KIAS.

10,500 pounds (4763 kilograms) and above GW – V

80 KIAS.

Engine torque greater than 49 PSI (88%) – V

80 KIAS.

Doors open/off operation – V

100 KIAS unless V

Placard (Figure 1-6A) is

more restrictive.

decreases linearly from 125 knots to 105 knots (Refer to Placards and

Decals, Figure 1-6A).

decreases 3 knots per 1000 feet above 3000 feet H

Maximum allowable tailwind is 20 knots when operating above 10,500 Lbs.

Maximum allowable tailwind is 30 knots when operating below 10,500 Lbs.

Maximum allowable crosswind is 30 knots.

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HP d212 Manual do Utilizador Página 21